CN109895418A - A kind of processing method of abnormity hollow structure composite material parts molding core model - Google Patents

A kind of processing method of abnormity hollow structure composite material parts molding core model Download PDF

Info

Publication number
CN109895418A
CN109895418A CN201910239803.5A CN201910239803A CN109895418A CN 109895418 A CN109895418 A CN 109895418A CN 201910239803 A CN201910239803 A CN 201910239803A CN 109895418 A CN109895418 A CN 109895418A
Authority
CN
China
Prior art keywords
soft mode
molding
die body
processing method
blank
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201910239803.5A
Other languages
Chinese (zh)
Other versions
CN109895418B (en
Inventor
李书军
陈剑
尹军华
李璐璐
杨自燕
周才超
石小平
任贵川
谷雨
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chengdu Union Aviation Technology Co Ltd
Original Assignee
Chengdu Union Aviation Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Chengdu Union Aviation Technology Co Ltd filed Critical Chengdu Union Aviation Technology Co Ltd
Priority to CN201910239803.5A priority Critical patent/CN109895418B/en
Publication of CN109895418A publication Critical patent/CN109895418A/en
Application granted granted Critical
Publication of CN109895418B publication Critical patent/CN109895418B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Moulds For Moulding Plastics Or The Like (AREA)

Abstract

The present invention relates to resin base fiber reinforced composite material prepreg autoclave molding technical fields, more particularly to a kind of processing method of special-shaped hollow structure composite material parts molding core model, it uses mandrel molding mold, there is molding space on mandrel molding mold, molding space is for forming mandrel molding, the wall surface of molding space is molded surface, comprising the following steps: will be on soft mode blank laying to molded surface;It pressurizes to soft mode blank and mandrel molding mold, is in close contact soft mode blank and mandrel molding mold;Solidify soft mode blank, forms soft mode;Water-soluble material is poured into soft mode, until soft mode inner cavity is completely filled;Solidify water-soluble material;Demoulding.The molding core mold that the above processing method provided through the invention obtains has that the processing is simple, is convenient in demoulding, the advantages of cost is relatively low.

Description

A kind of processing method of abnormity hollow structure composite material parts molding core model
Technical field
The present invention relates to resin base fiber reinforced composite material prepreg autoclave molding technical fields, especially a kind of The processing method of special-shaped hollow structure composite material parts molding core model.
Background technique
Composite material flies due to the features such as its light weight, specific strength and specific stiffness are high, designability is strong in aerospace Row device structural member field using increasingly extensive;But the manufacture of the hollow rotary structure composite material parts of abnormity is always Problem, such as the aero-engine air intake duct of S-shaped variable cross-section;The type constitutional detail generally selects surface quality and essence when forming Demanding one side is spent as the face being bonded with mold, abbreviation mold face.When the interior shape face of part is mold face, can be selected Formpiston laying and forming method, the demoulding after part solidifies are more difficult;When External Shape face is mold face, group can be selected Box-like former, then cannot be straight when no material prepreg laying space but if part section is small in order to subsequent demoulding Connect laying and molding on former, it is necessary to part is taken off from formpiston and is transferred on former in formpiston upper berth poststack solidifies, Uncured part blank demoulds more difficult from formpiston at this time.To achieve the purpose that smooth forming part, it is necessary to design A kind of easily demoulding molding core model;The molding core model mode usually used at present is as follows:
1) metallic combination formula forms core model, and molding core model assembly relation is more, and mating surface precision is high, and difficulty of processing is big, cost Height, and not can guarantee the whole air-tightness of mold, easily occur the problems such as vacuum leak in the curing process;When shape is more multiple When miscellaneous, the processing of metallic combination formula pattern be cannot achieve;
2) water-soluble molding core model: water solubility molding core model is divided into two kinds, and one kind is that pouring type forms core model, i.e., in type Molding core model is obtained after pouring special water-soluble material material solidification in chamber, such molding core model internal soundness and external mass It is required that it is high, it is unable to hole, material expensive, forming core mould manufacturing cost height;Another kind molding core model in type chamber by pouring At cube or cylindrical body, then by numerical control processing mode obtain molding core model face, such molding core model internal soundness and External mass requires height, is unable to hole, and require material machinable, same material expensive, and forming core mould manufacturing cost is high;
Water solubility molding core model could be simply possible to use in male mould forming by water-soluble removal only after part is fully cured, Be not suitable for external surface surface quality and the high variable cross-section hollow rotary structure composite material parts of abnormity of required precision at Type.
Summary of the invention
Goal of the invention of the invention is: for adding for special-shaped hollow structure composite material parts of the existing technology The problem that during work, mold cost is high, demoulding is difficult provides a kind of special-shaped hollow structure composite material parts molding core model Processing method, this processing method can be used in processing a kind of molding core model of easily demoulding composite material parts.
To achieve the goals above, the technical solution adopted by the present invention are as follows:
A kind of processing method of abnormity hollow structure composite material parts molding core model, it is described using mandrel molding mold There is molding space, for forming mandrel molding, the wall surface of the molding space is the molding space on mandrel molding mold Molded surface, comprising the following steps: will be on soft mode blank laying to the molded surface;To soft mode blank and mandrel molding mould Tool pressurizes, and is in close contact soft mode blank and mandrel molding mold;Solidify the soft mode blank, forms soft mode;To soft mode In pour water-soluble material, until soft mode inner cavity is completely filled;Solidify the water-soluble material;Demoulding.
The above processing method provided through the invention can process a kind of outer surface and be soft mode, be filled in inner cavity The molding core model of water-soluble material, when carrying out the processing of special-shaped hollow structure composite material parts by this molding core model, The surface laying carbon fibre composite layer of the molding core model, to composite layer solidification after, by water wash away removal it is water-soluble Property molding core model, be then deformed soft mode, demoulding can be realized.The molding core mold obtained by this processing method Have that the processing is simple, is convenient in demoulding, the advantages of cost is relatively low.
As a preferred solution of the present invention, the mandrel molding mold include the first die body and the second die body, described first Die body and second die body are detachably connected, and first die body and second die body form institute in connected state State molding space;After the completion of the demoulding step, the processing method is further comprising the steps of: repairing and cuts soft mode in the first mould The overlap formed at body and the second die body molding.Mandrel molding mold provided by the invention is set as above-mentioned structure, is processing It, can be convenient for the separation of molding core model and mandrel molding mold during the molding core model.
As a preferred solution of the present invention, the soft mode blank includes outer rubber layer, the carbon fibre initial rinse bed of material and interior rubber Layer;When by soft mode blank laying to the molded surface, first laying outer rubber layer repaves the folded carbon fibre initial rinse bed of material, most Laying inner rubber layer afterwards;Above-mentioned steps carry out respectively on the first die body and the second die body, right after the completion of soft mode blank laying First die body and the second die body are molded.By above-mentioned structure, the carbon fibre initial rinse bed of material is used to play the role of sizing, Guarantee soft mode under the effect of external force, the deflection of profile can control in appropriate range.Rubber layer setting and carbon fiber On the outside of prepreg, for protecting the carbon fibre initial rinse bed of material, the carbon fibre initial rinse bed of material is avoided thoroughly to be broken.
As a preferred solution of the present invention, the laying thickness of the carbon fibre initial rinse bed of material is not more than two layers of prepreg, often The thickness of layer prepreg is no more than 0.25mm.The thickness of the carbon fibre initial rinse bed of material to soft mode in this way, can either provide certain Styling, and enable to the shape of soft mode that can change, so that the process of the demoulding in composite material parts In, soft mode can be taken out and deforming soft mode.
As a preferred solution of the present invention, solidifying the soft mode blank, when forming soft mode, by soft mode blank and core model Molding die is integrally sent into autoclave, and vacuum, pressure are applied, and is warming up to needed for the vulcanization of rubber and carbon fiber prepreg solidification Temperature.
As a preferred solution of the present invention, in molding, the soft mode blank at molding is made to generate overlap joint.Make the first die body Overlap joint is generated with the soft mode blank at the second die body molding, can guarantee quality of the soft mode at molding.
As a preferred solution of the present invention, to soft mode blank and mandrel molding mold under pressure: in soft mode base The outside of the first die body and the second die body after material, molding is successively arranged with hole isolation film, airfelt and vacuum bag, by close Seal strip seals the vacuum bag, forms vacuum system, vacuumizes to the vacuum system;After the completion of pressurization, dismounting has hole isolation Film, airfelt, vacuum bag and sealing joint strip.By aforesaid operations, soft mode blank can be allowed sufficiently to paste with mandrel molding mold It closes, to guarantee soft mode blank surface quality after molding, so that composite material parts inner surface matter with higher Amount.
As a preferred solution of the present invention, solidifying the soft mode blank, formed in soft mode, after soft mode blank, molding The first die body and the outside of the second die body be successively arranged non-porous release film, airfelt and vacuum bag, sealed by sealing joint strip The vacuum bag is evacuated to vacuum degree not less than -0.9bar.
As a preferred solution of the present invention, the both ends of the molding space all have opening, and the mandrel molding mold is also Including sealing plate, for the sealing plate for being connected with the open edge, the sealing plate is equipped with through-hole;The molding core model includes Support rod, the support rod are adapted to the opening;Before being poured water-soluble material into soft mode, it is fitted into a sealing plate, It is inserted into support rod in the through hole of the sealing plate, described support rod one end is located in the water-soluble molding core model, other end position In outside the molding space, gap between gap, sealing plate and the second die body between sealing plate and the first die body, sealing plate are sealed Gap between support rod;Water-soluble material is being poured into soft mode, until installation is another after soft mode inner cavity is completely filled One sealing plate is inserted into support rod in the through hole of the sealing plate, and described support rod one end is located in the water-soluble core, separately One end is located at outside the molding space, seals the seam between gap, sealing plate and the second die body between sealing plate and the first die body Gap between gap, sealing plate and support rod.Meanwhile support rod is arranged on molding core model by setting, so that in following process During composite material parts, the molding core model can be fixed by support rod, to will not influence the table of molding core model Face is convenient for laying operation.
As a preferred solution of the present invention, when solidifying the water-soluble material, by mandrel molding mold, soft mode blank It is integrally placed in baking oven, heats up with water-soluble material, solidify water-soluble material.
In conclusion by adopting the above-described technical solution, the beneficial effects of the present invention are:
The above processing method provided through the invention can process a kind of outer surface and be soft mode, be filled in inner cavity The molding core model of water-soluble material, when carrying out the processing of special-shaped hollow structure composite material parts by this molding core model, The surface laying carbon fibre composite layer of the molding core model, to composite layer solidification after, by water wash away removal it is water-soluble Property molding core model, be then deformed soft mode, demoulding can be realized.The molding core mold obtained by this processing method Have that the processing is simple, is convenient in demoulding, the advantages of cost is relatively low.
Detailed description of the invention
Fig. 1 is a kind of structural representation of variable cross-section abnormity hollow structure composite material parts provided in an embodiment of the present invention Figure.
Fig. 2 is the structural schematic diagram of mandrel molding mold provided in an embodiment of the present invention.
Fig. 3 is structural schematic diagram when mandrel molding mold provided in an embodiment of the present invention removes sealing plate.
Fig. 4 is to carry out structural schematic diagram when step S3 in processing method provided in an embodiment of the present invention.
Fig. 5 is the partial enlarged view in the portion I in Fig. 4.
Fig. 6 is to carry out structural schematic diagram when step S4 in processing method provided in an embodiment of the present invention.
Fig. 7 is the structural schematic diagram in processing method provided in an embodiment of the present invention, after the completion of step S6.
Fig. 8 is the structural schematic diagram for the molding core model that the processing method provided through the embodiment of the present invention obtains.
Fig. 9 is the cross-sectional view for the molding core model that the processing method provided through the embodiment of the present invention obtains.
Figure 10 is the schematic diagram that the pre-compacted in processing instance (one), when carrying out step A3 operates.
Figure 11 is II in Figure 10 partial enlarged view.
Figure 12 is to carry out schematic diagram when step A4 in processing instance (one).
Figure 13 is III in Figure 12 partial enlarged view.
Figure 14 is the structural schematic diagram for the shaping female mold used in processing instance (two).
Figure 15 is to carry out structural schematic diagram when step B3 in processing instance (two).
Figure 16 is to carry out structural schematic diagram when step B6 in processing instance (two).
Icon: 1- composite material parts;2- mandrel molding mold;The first die body of 21-;The second die body of 22-;23- sealing plate; 4- has hole isolation film;5- airfelt;6- vacuum bag;7- non-porous release film;8- sealing joint strip;3- forms core model;31- soft mode; 32- water solubility core;33- support rod;9- shaping female mold;The first former die body of 91-;The second former die body of 92-.
Specific embodiment
With reference to the accompanying drawing, the present invention is described in detail.
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to the accompanying drawings and embodiments, The present invention will be described in further detail.It should be appreciated that described herein, specific examples are only used to explain the present invention, It is not intended to limit the present invention.
Embodiment
Please refer to Fig. 1-Fig. 9.The embodiment of the invention provides a kind of hollow rotary structure composite materials of variable cross-section abnormity The processing method of the molding core model 3 of part 1.Fig. 8 and Fig. 9 is please referred to, this processing method can obtain a kind of molding core model 3.This Kind molding core model 3 can be used in processing the hollow rotary structure composite material parts 1 of variable cross-section abnormity as shown in Figure 1.
Please refer to figs. 2 and 3, processing method provided in an embodiment of the present invention use mandrel molding mold 2, the core model at Pattern tool 2 includes the first die body 21, the second die body 22 and sealing plate 23.First die body 21 and the second die body 22 are detachably connected. When first die body 21 is connected with the second die body 22, it is capable of forming molding space, the shape of molding space is used for and the composite material The outer surface of part 1 is adapted to.The both ends of molding space are equipped with opening, and the opening is for being in communication with the outside.The table of molding space Face is molded surface.
Wherein, in the present embodiment, the first die body 21 is detachably connected with the second die body 22 by screw realization.
The quantity of sealing plate 23 is two, and one of sealing plate 23 is used to be connected with the opening of molding space one end, another Sealing plate 23 with the opening of the molding space other end for being connected.Sealing plate 23 is equipped with through-hole.
Processing method provided in an embodiment of the present invention the following steps are included:
It S1. will be on 31 blank laying to the molded surface of soft mode;
Wherein, 31 blank of soft mode includes outer rubber layer, the carbon fibre initial rinse bed of material and inner rubber layer.During laying, Outer rubber layer, the carbon fibre initial rinse bed of material and inner rubber layer are successively laid on the molded surface on the first die body 21, in the second mould Outer rubber layer, the carbon fibre initial rinse bed of material and inner rubber layer are successively laid on the molded surface of body 22.
Further, in the present embodiment, the solidification temperature of the carbon fibre initial rinse bed of material and outer rubber layer and inner rubber layer Curing temperature is close, so that the carbon fibre initial rinse bed of material can sufficiently solidify during cured later, rubber layer being capable of abundant sulphur Change.
Further, in the present embodiment, the carbon fibre initial rinse bed of material is carbon fibre fabric prepreg.Outer rubber layer and The rubber material that inner rubber layer selects heatproof to be more than or equal to 250 DEG C, sulfurizing temperature range are 176 ± 5 DEG C.
Wherein, the thickness of two layers of the laying layer number of carbon fiber prepreg, the single layer carbon fibre initial rinse bed of material is no more than 0.25mm.The laying direction of two layers of carbon fibre fabric prepreg is consistent, and to guarantee the symmetry of laying, avoids carbon fiber Dimension prepreg deforms after hardening.
S2. die closing operation is carried out to the first die body 21 and the second die body 22;
Wherein, at molding, produce 31 blank of soft mode on 31 blank of soft mode and the second die body 22 on the first die body 21 Raw overlap joint, to increase intensity of the soft mode 31 at molding.
Please refer to Fig. 4 and Fig. 5:
S3. it pressurizes to 31 blank of soft mode and mandrel molding mold 2, keeps 31 blank of soft mode and mandrel molding mold 2 tight Contiguity touching;
Wherein, the outside of the first die body 21 after 31 blank of soft mode, molding and the second die body 22 be successively arranged with hole every From film 4, airfelt 5 and vacuum bag 6, the vacuum bag 6 is sealed by sealing joint strip 8, vacuum system is formed, to the vacuum system System vacuumizes, to generate pressure, is in close contact 31 blank of soft mode and the first die body 21 and the second die body 22.
After the completion of pressurization, removal has hole isolation film 4, airfelt 5 and vacuum bag 6.
Please refer to Fig. 6 and Fig. 7:
S4. solidify 31 blank of soft mode, form soft mode 31;
Wherein, the outside of the first die body 21 after 31 blank of soft mode, molding and the second die body 22 be successively arranged it is non-porous every From film 7, airfelt 5 and vacuum bag 6, the vacuum bag 6 is sealed by sealing joint strip 8, be evacuated to vacuum degree not less than- 0.9bar applies in 31 blank of soft mode and the whole feeding autoclave of mandrel molding mold 2 vacuum, pressure, is warming up to rubber Vulcanization and the carbon fibre initial rinse bed of material solidify required temperature;
After the completion of solidification, removal non-porous release film 7, airfelt 5 and vacuum bag 6.
S5. it is fitted into a sealing plate 23, is inserted into support rod 33 in the through hole of sealing plate 23,33 one end of support rod is located at In the molding space, the other end is located at outside the molding space, seals the gap between sealing plate 23 and the first die body 21, seals Gap, sealing plate 23 between plate 23 and the second die body 22 and the gap between support rod 33;
Wherein, by sealing joint strip 8 to being sealed at each gap.
S6. water-soluble material is poured into soft mode 31, until 31 inner cavity of soft mode is completely filled.
Water-soluble material in the present embodiment refers to, the material that can be removed under the souring of water flow.In this reality It applies in example, it is preferred to use water-soluble material resistant to high temperature, such as: polyvinyl alcohol (PVAL) aqueous solution and polyvinylpyrrolidone (PVP) mixed solution of aqueous solution is as basis material, using quartz sand or glass microballoon as the water-soluble material of reinforcing material. Wherein the mixed solution of polyvinyl alcohol (PVAL) aqueous solution and polyvinylpyrrolidone (PVP) aqueous solution is as adhesive, the glue Stick is water-soluble.After adhesive meets water dissolution, quartz sand or glass microballoon will be defeated and dispersed, to make water-soluble core It is removed.
S7., another sealing plate 23 is installed, is inserted into support rod 33 in the through hole of sealing plate 23,33 one end of support rod is located at water In soluble materials, the other end is located at outside molding space, seals gap between sealing plate 23 and the first die body 21, sealing plate 23 and the Gap, sealing plate 23 between two die bodys 22 and the gap between support rod 33.
S8. solidify the water-soluble material;
Wherein, mandrel molding mold 2,31 blank of soft mode and water-soluble material are integrally placed in baking oven, are heated up, Solidify water-soluble material.
S9. it demoulds.
Sealing plate 23 is removed, separates the first die body 21 with the second die body 22.
S10. the overlap for cutting soft mode 31 at molding is repaired.
The molding core model 3 that the above-mentioned processing method provided through the embodiment of the present invention obtains includes soft mode 31, Water-Soluble Core Portion 32 and support rod 33.
Wherein, soft mode 31 includes the outer rubber layer and inner rubber layer of vulcanization, is carbon between outer rubber layer and inner rubber layer Fiber composite layer.The water solubility core 32 made of water-soluble material is filled in the space that soft mode 31 surrounds.
The quantity of support rod 33 is two, and one of support rod 33 is located at one end of water-soluble core 32, another branch Strut 33 is located at the other end of water-soluble core 32.33 one end of support rod is inserted into water-soluble core 32, and the other end is located at water Except dissolubility core 32.
The molding core model 3 obtained by above-mentioned processing method, can either be used for inner mold face surface quality and required precision is high The hollow rotary structure composite material parts 1 of variable cross-section abnormity processing, and can be used in outer mold surface surface quality and precision The processing of the hollow rotary structure composite material parts 1 of demanding variable cross-section abnormity.
It is illustrated below by way of two processing instances:
Processing instance (one):
Figure 10-Figure 13 is please referred to, when the change high for inner mold face surface quality and required precision of above-mentioned molding core model 3 When the processing of cross section special-shaped hollow rotary structure composite material parts 1:
A1. the molding core model 3 is fixed by support rod 33;
Wherein, the fixation of molding core model 3 can be realized, so that entire 31 surface of soft mode be made not hidden in clamp standoff bar 33 Gear, is convenient for the paving of composite layer.
A2. in the surface paving band glue release cloth of soft mode 31;
31 surface of soft mode could be covered if necessary to muti-piece release cloth, then is docked between adjacent two pieces of release cloths, without spelling It connects.That is: the sideline of two pieces of adjacent release cloths is in contact, but two pieces of release cloths do not generate overlapping in a thickness direction.Pass through this Kind setting influences the surface quality of composite material parts 1 after avoiding release cloth from being overlapped.
A3. in the 31 surface paving material prepreg of soft mode;
Wherein, during paving, a pre-compacted is carried out every preset thickness of composite material.Pre-compacted operation It is specifically performed such that on the outside of composite layer and is successively equipped with hole isolation film 4, airfelt 5 and vacuum bag 6, seal vacuum bag 6, it is located at molding die and composite material in vacuum bag 6, to form vacuum system, which is vacuumized, by big The effect of air pressure is compacted composite material.
Further, after laying for the first time and subsequent every three layings, carry out a pre-compacted operation.
A4. solidify the material prepreg;
Wherein, in this way carry out material prepreg solidification: be successively laid on the outside of the composite layer it is non-porous every From film 7, airfelt 5 and vacuum bag 6, the vacuum bag 6 is sealed, the molding die and composite material is made to be located at the vacuum In bag 6, to form vacuum system, the vacuum system is integrally placed in autoclave, applies pressure, vacuum, increases temperature.
A5. the water-soluble core 32, separation soft mode 31 and cured composite material are removed;
Wherein, which is rinsed by the water flow of giant, after removing water-soluble core 32, makes soft mode 31 are deformed, separation soft mode 31 and cured composite material.
A6. the composite material after solidification repair and cut processing, obtain required composite material parts 1.
Processing instance (two)
Figure 14-Figure 16 is please referred to, when the change high for outer mold surface surface quality and required precision of above-mentioned molding core model 3 When the processing of cross section special-shaped hollow rotary structure composite material parts 1:
B1. the molding core model 3 is fixed by support rod 33;
Wherein, the fixation of molding core model 3 can be realized, so that entire 31 surface of soft mode be made not hidden in clamp standoff bar 33 Gear, is convenient for the paving of composite layer.
B2. in the surface paving band glue release cloth of soft mode 31;
31 surface of soft mode could be covered if necessary to muti-piece release cloth, then is docked between adjacent two pieces of release cloths, without spelling It connects.That is: the sideline of two pieces of adjacent release cloths is in contact, but two pieces of release cloths do not generate overlapping in a thickness direction.Pass through this Kind setting influences the surface quality of composite material parts 1 after avoiding release cloth from being overlapped.
B3. in the 31 surface paving material prepreg of soft mode;
Wherein, during paving, a pre-compacted is carried out every preset thickness of composite material.Pre-compacted operation It is specifically performed such that on the outside of composite layer and is successively equipped with hole isolation film 4, airfelt 5 and vacuum bag 6, seal vacuum bag 6, it is located at molding die and composite material in vacuum bag 6, to form vacuum system, which is vacuumized, by big The effect of air pressure is compacted composite material.
Further, after laying for the first time and subsequent every three layings, carry out a pre-compacted operation.
After the completion of pre-compacted operation, removal has hole isolation film 4, airfelt 5 and vacuum bag 6.
B4. sealing joint strip 8 is arranged in the region of non-mulching composite prepreg on 31 surface of soft mode, on soft mode 31 Covering vacuum bag 6 makes sealing joint strip 8, vacuum bag 6 and soft mode 31 form a sealing system, and material prepreg is located at should In sealing system.
B5. the water-soluble core 32 is removed.
Wherein it is possible to wash off water-soluble core 32 by giant.After removing water-soluble core 32, wipe soft 31 inner surface of mould.
B6. soft mode 31, material prepreg are placed in shaping female mold 9, solidify material prepreg;
Wherein, when solidifying material prepreg, it is successively laid with non-porous release film 7 on the outside of composite layer, breathes freely Felt 5 and vacuum bag 6 seal the vacuum bag 6, and molding core model 3, shaping female mold 9 and composite material is made to be located at the vacuum bag 6 In, to form vacuum system, vacuum system is integrally placed in autoclave, applies pressure, vacuum, increases temperature.
B7. the first former die body 91 and the second former die body 92 are dismantled, soft mode 31 is removed;
B8. it polishes on composite material parts 1, at 92 molding of the first former die body 91 and the second former die body Glue rib, repairs and cuts shape, composite material parts 1 required for obtaining.
The processing method of the hollow rotary structure composite material parts 1 of variable cross-section abnormity provided by the invention has following The utility model has the advantages that
1. the above processing method provided through the invention, a kind of outer surface can be processed and be soft mode 31, fill out in inner cavity Molding core model 3 filled with water-soluble material carries out adding for special-shaped hollow structure composite material parts 1 by this molding core model 3 Working hour passes through washing away for water after composite layer solidification in the surface laying carbon fibre composite layer of the molding core model 3 The water-soluble molding core model 3 of removal, is then deformed soft mode 31, demoulding can be realized.It is obtained by this processing method Core model 3 has the advantages that the processing is simple, is convenient in demoulding, cost is relatively low for molding.
2. in processing method provided in an embodiment of the present invention, including carbon fibre composite layer in soft mode 31, capable of giving Soft mode 31 provides certain style-ability, and soft mode 31 is avoided to generate excessively big deformation, while the carbon fiber being laid with further through control The thickness for tieing up composite layer, allows the shape of soft mode 31 to change, consequently facilitating demoulding;
3. in processing method provided by the invention, carbon fibre composite layer is set between inner rubber layer and outer rubber layer, Carbon fibre composite layer can be formed by inner rubber layer and outer rubber layer and be protected, so that even if carbon fibre composite Local damage has occurred in layer, and the thorough fracture of soft mode 31 will not be caused due to the local damage.
It should be noted that simply showing a kind of possible feelings of 1 structure of composite material parts in attached drawing of the invention Shape.Processing method provided by the invention can also be used to the processing of the molding core model 3 of other different structures, be not limited solely to attached A kind of situation shown in figure.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention Made any modifications, equivalent replacements, and improvements etc., should all be included in the protection scope of the present invention within mind and principle.

Claims (10)

1. a kind of processing method of abnormity hollow structure composite material parts molding core model, which is characterized in that use mandrel molding Mold, has molding space on the mandrel molding mold, and the molding space is used to form the molding of core model, the molding sky Between wall surface be molded surface, comprising the following steps:
It will be on soft mode blank laying to the molded surface;
It pressurizes to soft mode blank and mandrel molding mold, is in close contact soft mode blank and mandrel molding mold;
Solidify the soft mode blank, forms soft mode;
Water-soluble material is poured into soft mode, until soft mode inner cavity is completely filled;
Solidify the water-soluble material;
Demoulding.
2. processing method according to claim 1, which is characterized in that the mandrel molding mold includes the first die body and the Two die bodys, first die body and second die body are detachably connected, and first die body and second die body are even It connects and forms the molding space under state;
After the completion of the demoulding step, the processing method is further comprising the steps of:
It repairs and cuts the overlap that soft mode is formed at the first die body and the second die body molding.
3. processing method according to claim 2, which is characterized in that the soft mode blank includes outer rubber layer, carbon fiber Prepreg and inner rubber layer;
When by soft mode blank laying to the molded surface, first laying outer rubber layer repaves the folded carbon fibre initial rinse bed of material, most Laying inner rubber layer afterwards;
Above-mentioned steps carry out respectively on the first die body and the second die body, after the completion of soft mode blank laying, to the first die body and Two die bodys are molded.
4. processing method according to claim 3, which is characterized in that the laying thickness of the carbon fibre initial rinse bed of material is little It is no more than 0.25mm in the thickness of two layers of prepreg, every layer of prepreg.
5. processing method according to claim 3, which is characterized in that solidifying the soft mode blank, it, will when forming soft mode Soft mode blank and mandrel molding mold are integrally sent into autoclave, are applied vacuum, pressure, are warming up to the vulcanization of rubber and carbon fiber is pre- Leaching material solidification required temperature.
6. processing method according to claim 3, which is characterized in that in molding, generate the soft mode blank at molding Overlap joint.
7. processing method according to claim 6, which is characterized in that whole to soft mode blank and the progress of mandrel molding mold When body vacuumizes pre-compacted:
The outside of the first die body and the second die body after soft mode blank, molding is successively arranged with hole isolation film, airfelt and true Empty bag seals the vacuum bag by sealing joint strip, forms vacuum system, vacuumize to the vacuum system;
After the completion of vacuumizing pre-compacted, dismounting has hole isolation film, airfelt, vacuum bag and sealing joint strip.
8. processing method according to claim 7, which is characterized in that solidifying the soft mode blank, is being formed in soft mode, The outside of the first die body and the second die body after soft mode blank, molding is successively arranged non-porous release film, airfelt and vacuum bag, leads to It crosses sealing joint strip and seals the vacuum bag, be evacuated to vacuum degree not less than -0.9bar.
9. processing method according to claim 1, which is characterized in that the both ends of the molding space all have opening, institute Stating mandrel molding mold further includes sealing plate, and for the sealing plate for being connected with the open edge, the sealing plate is equipped with through-hole;
The molding core model includes support rod, and the support rod is adapted to the opening;
Before being poured water-soluble material into soft mode, it is fitted into a sealing plate, is inserted into support rod in the through hole of the sealing plate, Described support rod one end is located in the molding space, and the other end is located at outside the molding space, seals sealing plate and the first die body Between gap, the gap between sealing plate and the second die body, the gap between sealing plate and support rod;
Water-soluble material is being poured into soft mode, until another sealing plate is installed, in the envelope after soft mode inner cavity is completely filled Support rod is inserted into the through hole of plate, and described support rod one end is located in the water-soluble material, and it is empty that the other end is located at the molding Between it is outer, seal between gap, sealing plate and the support rod between gap, sealing plate and the second die body between sealing plate and the first die body Gap.
10. processing method according to claim 9, which is characterized in that when solidifying the water-soluble material, by core model at Pattern tool, soft mode blank and water-soluble material are integrally placed in baking oven, are heated up, are made water-soluble material baking and curing.
CN201910239803.5A 2019-03-27 2019-03-27 Processing method of special-shaped hollow structure composite material part forming core mold Active CN109895418B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910239803.5A CN109895418B (en) 2019-03-27 2019-03-27 Processing method of special-shaped hollow structure composite material part forming core mold

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910239803.5A CN109895418B (en) 2019-03-27 2019-03-27 Processing method of special-shaped hollow structure composite material part forming core mold

Publications (2)

Publication Number Publication Date
CN109895418A true CN109895418A (en) 2019-06-18
CN109895418B CN109895418B (en) 2021-02-19

Family

ID=66953935

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910239803.5A Active CN109895418B (en) 2019-03-27 2019-03-27 Processing method of special-shaped hollow structure composite material part forming core mold

Country Status (1)

Country Link
CN (1) CN109895418B (en)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110253792A (en) * 2019-07-30 2019-09-20 哈尔滨市航科技术开发有限责任公司 Wind-tunnel loss of weight model aircraft composite material sends out room component core-pulling type mold
CN111873484A (en) * 2020-07-14 2020-11-03 菲舍尔航空部件(镇江)有限公司 Manufacturing method of pressure pad for forming aviation glass fiber composite part
CN113103622A (en) * 2021-05-14 2021-07-13 天津爱思达新材料科技有限公司 Forming method and mould device for composite material thin-wall fuel tank with hollow ring frame
CN113232328A (en) * 2021-03-31 2021-08-10 成都飞机工业(集团)有限责任公司 Manufacturing method of composite material S-shaped air inlet duct cylinder based on 2.5D weaving
CN113910637A (en) * 2021-10-11 2022-01-11 航天特种材料及工艺技术研究所 Forming method of composite material complex special-shaped air inlet channel
CN113927919A (en) * 2021-10-27 2022-01-14 陕西天翌天线股份有限公司 Forming method of environment-controlled catheter
CN113954274A (en) * 2021-10-27 2022-01-21 陕西天翌天线股份有限公司 Method for manufacturing core mold
CN114131796A (en) * 2021-10-29 2022-03-04 中国船舶重工集团公司第七二五研究所 Manufacturing method and application of light-weight high-strength male mold suitable for large-scale composite material structural member
CN114193790A (en) * 2021-12-01 2022-03-18 长春长光宇航复合材料有限公司 Forming method for composite material reinforced shell cabin sections of different resin systems
CN114274552A (en) * 2021-11-24 2022-04-05 常州启赋安泰复合材料科技有限公司 Forming die and processing method of composite material transmission shaft
CN114834062A (en) * 2022-03-29 2022-08-02 天津爱思达新材料科技有限公司 Forming process of special-shaped airplane air inlet channel
CN115090831A (en) * 2022-06-14 2022-09-23 南京航空航天大学 Composite material special-shaped revolving body forming method based on 3D printing lightweight sand mold
CN115107296A (en) * 2022-06-10 2022-09-27 中国人民解放军总参谋部第六十研究所 Die and method for integrally forming head conical part with smooth inner and outer surfaces
CN115674510A (en) * 2022-11-26 2023-02-03 零八一电子集团四川天源机械有限公司 Manufacturing method of detachable core mold of composite hollow structure product
CN117162539A (en) * 2023-11-02 2023-12-05 成都泰格尔航天航空科技股份有限公司 Compacting device and production process thereof

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0492129A1 (en) * 1990-11-26 1992-07-01 Excell Corporation A multi-layer plastic pipe and its method for manufacturing
CN101585236A (en) * 2008-05-23 2009-11-25 珠海市恒基业安全头盔有限公司 Molding technology of composite material special product
CN101890807A (en) * 2010-07-19 2010-11-24 哈尔滨飞机工业集团有限责任公司 Method for pressurizing and molding composite part by using thermal expansion of silicone rubber
US20140103561A1 (en) * 2012-10-15 2014-04-17 Jiin-Biau Huang Method for molding composite material
CN104441696A (en) * 2014-09-22 2015-03-25 成都飞机工业(集团)有限责任公司 Manufacture method of special-shaped composite material rib
CN106166811A (en) * 2016-07-01 2016-11-30 宜兴市凯诚模具有限公司 A kind of production technology of silica gel mould
CN106313378A (en) * 2016-10-11 2017-01-11 中国航空工业集团公司基础技术研究院 Method for preparing and using fiber-reinforced hat-shaped rib molding soft mold
CN108115948A (en) * 2017-12-26 2018-06-05 天津工业大学 A kind of composite material shaping core and preparation method
CN108943769A (en) * 2018-06-21 2018-12-07 西安爱生技术集团公司 The manufacturing method of the non-isometrical enclosed type square tube type carbon fiber girder construction product of unmanned plane
JP2019025848A (en) * 2017-08-02 2019-02-21 藤倉ゴム工業株式会社 Method for manufacturing hollow elastic molding

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0492129A1 (en) * 1990-11-26 1992-07-01 Excell Corporation A multi-layer plastic pipe and its method for manufacturing
CN101585236A (en) * 2008-05-23 2009-11-25 珠海市恒基业安全头盔有限公司 Molding technology of composite material special product
CN101890807A (en) * 2010-07-19 2010-11-24 哈尔滨飞机工业集团有限责任公司 Method for pressurizing and molding composite part by using thermal expansion of silicone rubber
US20140103561A1 (en) * 2012-10-15 2014-04-17 Jiin-Biau Huang Method for molding composite material
CN104441696A (en) * 2014-09-22 2015-03-25 成都飞机工业(集团)有限责任公司 Manufacture method of special-shaped composite material rib
CN106166811A (en) * 2016-07-01 2016-11-30 宜兴市凯诚模具有限公司 A kind of production technology of silica gel mould
CN106313378A (en) * 2016-10-11 2017-01-11 中国航空工业集团公司基础技术研究院 Method for preparing and using fiber-reinforced hat-shaped rib molding soft mold
JP2019025848A (en) * 2017-08-02 2019-02-21 藤倉ゴム工業株式会社 Method for manufacturing hollow elastic molding
CN108115948A (en) * 2017-12-26 2018-06-05 天津工业大学 A kind of composite material shaping core and preparation method
CN108943769A (en) * 2018-06-21 2018-12-07 西安爱生技术集团公司 The manufacturing method of the non-isometrical enclosed type square tube type carbon fiber girder construction product of unmanned plane

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
徐竹: "《复合材料成型工艺及应用》", 31 January 2017 *

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110253792A (en) * 2019-07-30 2019-09-20 哈尔滨市航科技术开发有限责任公司 Wind-tunnel loss of weight model aircraft composite material sends out room component core-pulling type mold
CN111873484A (en) * 2020-07-14 2020-11-03 菲舍尔航空部件(镇江)有限公司 Manufacturing method of pressure pad for forming aviation glass fiber composite part
CN113232328A (en) * 2021-03-31 2021-08-10 成都飞机工业(集团)有限责任公司 Manufacturing method of composite material S-shaped air inlet duct cylinder based on 2.5D weaving
CN113103622B (en) * 2021-05-14 2022-04-26 天津爱思达新材料科技有限公司 Forming method and mould device for composite material thin-wall fuel tank with hollow ring frame
CN113103622A (en) * 2021-05-14 2021-07-13 天津爱思达新材料科技有限公司 Forming method and mould device for composite material thin-wall fuel tank with hollow ring frame
CN113910637B (en) * 2021-10-11 2023-04-11 航天特种材料及工艺技术研究所 Forming method of composite material complex special-shaped air inlet channel
CN113910637A (en) * 2021-10-11 2022-01-11 航天特种材料及工艺技术研究所 Forming method of composite material complex special-shaped air inlet channel
CN113927919A (en) * 2021-10-27 2022-01-14 陕西天翌天线股份有限公司 Forming method of environment-controlled catheter
CN113954274A (en) * 2021-10-27 2022-01-21 陕西天翌天线股份有限公司 Method for manufacturing core mold
CN114131796A (en) * 2021-10-29 2022-03-04 中国船舶重工集团公司第七二五研究所 Manufacturing method and application of light-weight high-strength male mold suitable for large-scale composite material structural member
CN114274552A (en) * 2021-11-24 2022-04-05 常州启赋安泰复合材料科技有限公司 Forming die and processing method of composite material transmission shaft
CN114274552B (en) * 2021-11-24 2023-11-10 常州启赋安泰复合材料科技有限公司 Forming die and processing method of composite material transmission shaft
CN114193790A (en) * 2021-12-01 2022-03-18 长春长光宇航复合材料有限公司 Forming method for composite material reinforced shell cabin sections of different resin systems
CN114193790B (en) * 2021-12-01 2024-02-20 长春长光宇航复合材料有限公司 Forming method of reinforced shell cabin section of composite material with different resin systems
CN114834062A (en) * 2022-03-29 2022-08-02 天津爱思达新材料科技有限公司 Forming process of special-shaped airplane air inlet channel
CN115107296A (en) * 2022-06-10 2022-09-27 中国人民解放军总参谋部第六十研究所 Die and method for integrally forming head conical part with smooth inner and outer surfaces
CN115090831A (en) * 2022-06-14 2022-09-23 南京航空航天大学 Composite material special-shaped revolving body forming method based on 3D printing lightweight sand mold
CN115674510A (en) * 2022-11-26 2023-02-03 零八一电子集团四川天源机械有限公司 Manufacturing method of detachable core mold of composite hollow structure product
CN117162539A (en) * 2023-11-02 2023-12-05 成都泰格尔航天航空科技股份有限公司 Compacting device and production process thereof
CN117162539B (en) * 2023-11-02 2024-02-06 成都泰格尔航天航空科技股份有限公司 Compacting device and production process thereof

Also Published As

Publication number Publication date
CN109895418B (en) 2021-02-19

Similar Documents

Publication Publication Date Title
CN109895418A (en) A kind of processing method of abnormity hollow structure composite material parts molding core model
CN109849371A (en) The variable cross-section hollow structure composite material parts forming method of high-precision inner surface
CN109895417A (en) The variable cross-section hollow structure composite material parts forming method of high-precision outer surface
CN103909658B (en) Composite material connecting skirt forming method and mold and inner rubber core mold forming mold
CN100436095C (en) Method for producing sealing rubber air-bag male die and resin transfer molding method therefor
KR101882535B1 (en) Methods and systems for co-bonding or co-curing composite parts using a rigid/malleable smp apparatus
CN107139514B (en) A kind of manufacturing method of air bag aided composite Material Stiffened Panel
EP2043832B1 (en) Method for producing a fibre composite component using a moulding core, and said moulding core
KR910000499B1 (en) Manufacturing method of hollow fiber reinforced structures
CN105235237A (en) Molding technology and molding tool of composite material J-shaped stiffened wallboard
US20150137424A1 (en) System and method for manufacturing monolithic structures using expanding internal tools
JPH03104799A (en) Manufacture of composite material blade
CN108943769A (en) The manufacturing method of the non-isometrical enclosed type square tube type carbon fiber girder construction product of unmanned plane
CN108891040B (en) Manufacturing method of composite horizontal tail wing of small and medium-sized unmanned aerial vehicle
CN103341987A (en) Co-curing process for omega-stringer vertical and horizontal reinforcement composite integral wallboard
CN112406135B (en) Method for assisting forming of composite propeller blade by air bag blowing
CN107521124A (en) Carbon fiber dual platen reinforced structure part and its manufacture method
WO2018133177A1 (en) Application of hsm process in wing moulding and method for moulding wing
CN105082568A (en) Liquid molding process of special-shaped composite structural part
JP4721251B2 (en) Manufacturing method of composite reinforcing plate
CN106273539A (en) A kind of shape for hat Material Stiffened Panel co-curing moulding technique
US20060220273A1 (en) Process for compression moulding liquid resins with structural reinforcements
CN105690791A (en) Barrel-shaped composite structural member overall molding method capable of achieving easy demolding
US7758793B2 (en) Method and apparatus for manufacturing of an article including an empty space
US4202856A (en) Graphite-epoxy molding method

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant